曝光台 注意防骗
网曝天猫店富美金盛家居专营店坑蒙拐骗欺诈消费者
only the following essential avionics receive adequate
cooling: FCC A, one AHRS, and the right
transformer rectifier. All other avionics systems are
susceptible to failure or shutdown due to heat. Ambient
temperature significantly influences the rate
at which avionics systems fail.
Bleed air leak MSP codes: 953, 954, 955, 956, 957,
958, 959, 960, or 961 (code determines leak location).
Over pressurization MSP code: 833.
INFLIGHT - DUAL
1. BLEED AIR knob - DO NOT CYCLE
2. Emergency oxygen green ring - PULL
3. MSP codes - CHECK for 953 to 961 and for
833.
If 833 present without 953 to 961 (over
pressure occurred) -
4. BLEED AIR knob - CYCLE THRU OFF to
NORM
If 953 to 961 are present (BALD shutdown)
or if both cauts return -
5. BLEED AIR knob - OFF (DO NOT CYCLE)
6. Maintain altitude below 10,000 feet.
7. Maintain airspeed below 325 KCAS (300 to 325
KCAS optimum).
8. ECS MODE switch - OFF/RAM
9. AV COOL switch - EMERG
Once below 10,000 feet -
10. Consider removing mask and resetting emergency
oxygen.
11. CABIN PRESS switch - RAM/DUMP
12. OXY FLOW knob - OFF
13. OBOGS control switch - OFF
14. Land as soon as practical.
If AV AIR HOT caution appears OR aft avionics
cooling fan disabled -
15. Non-essential avionics equipment - OFF (e.g.,
RADAR, UFCD controlled avionics, ECM, sensors,
MC2)
16. Land as soon as possible.
INFLIGHT - SINGLE
1. BLEED AIR knob affected engine - OFF (DO
NOT CYCLE)
2. Land as soon as practical
L BOOST LO
R BOOST LO
· Loss of fuel boost pressure to designated engine.
May result from prolonged transitions through
zero g (greater than 2 seconds). May also indicate
a fuselage fuel leak, fuel transfer failure, or
power transmission shaft failure (if accompanied
by the corresponding GEN, DC FAIL, and HYD
circuit cautions).
The crossfeed and cross cooling valves open automatically.
Afterburners may not operate above
30,000 feet.
1. Limit corresponding afterburner usage above
30,000 feet.
2. Check for indications of fuselage fuel leak.
3. Monitor fuel transfer.
4. Land as soon as practical.
A1-F18EA-NFM-000
Figure 12-1. Warning/Caution/Advisory Displays (Sheet 10 of 55)
V-12-12 ORIGINAL
DDI Cautions and Caution Lights
INDICATOR · CAUSE / REMARKS CORRECTIVE ACTION
BRK ACCUM
· Brake accumulator pressure low (below 2,000
psi).
A BRK ACCUM caution inflight is not normal
and may indicate a possible leak in the isolated
HYD 2B system. If the caution appears inflight,
do not attempt to recharge the accumulator as
this may result in additional loss of HYD 2B
fluid.
1. BRAKE PRESS gauge - CHECK
2. Extend landing gear as soon as practical.
IF HYD 2A caution also set -
3. Consider a short field arrested landing.
CANOPY
· Canopy not down and locked.
In the F/A-18F, rear seat occupant should lower
seat and lean as far forward as possible, in case the
canopy departs the aircraft.
INFLIGHT
1. CANOPY switch - CONFIRM DOWN
2. Slow below 300 KCAS, 200 KCAS in F/A-18F
(if practical)
3. Maintain altitude below 25,000 feet.
4. CABIN PRESS switch - RAM/DUMP
5. CANOPY switch - DOWN
6. CABIN PRESS switch - NORM
If light stays on -
7. Land as soon as practical.
CAUT DEGD
· Capability to display cautions degraded.
Displayed cautions may be false or erratic.
1. SDC - RESET
2. MC switch - CYCLE to 1 OFF then NORM
If caution remains or reappears -
3. Land as soon as practical.
CHECK SEAT
CK SEAT
Caution Light
· With WonW, one or both ejection seats are not
armed when both throttles are advanced beyond
27° THA.
1. Ejection set SAFE/ARMED handle(s) -
CHECK ARMED
CHECK TRIM
· With WonW, trim is not set for takeoff.
The caution is displayed when both throttles
are advanced beyond 27° THA if the stabilators
are trimmed less than 3.5° TEU with the launch
bar up (field takeoff) or 6.5° TEU with the
launch bar down (carrier takeoff).
1. T/O TRIM button - PRESS UNTIL TRIM
ADVISORY DISPLAYED (stabilators 4° NU)
If carrier-based -
2. TRIM - SET FOR CATAPULT LAUNCH
CK FLAPS
· With WonW, flaps are not set for takeoff.
The caution is displayed when both throttles
are advanced beyond 27° THA with the FLAP
switch in AUTO and the launch bar up (field
takeoff) or with the FLAP switch not in FULL
and the launch bar down (carrier takeoff).
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
本文链接地址：
NATOPS Flight Manual 飞行手册 2(21)
